发明名称 EBW TRIGGERING DEVICE FOR SATELLITE LAUNCH VEHICLE
摘要 An EBW(Exploding BridgeWire) triggering device for a satellite launch vehicle is provided to prevent excessive design of a system and reduce the manufacturing cost by charging a triggering capacitor by using constant voltage. An EBW(Exploding BridgeWire) triggering device for a satellite launch vehicle comprises a flyback conversion section(110) including a flyback transformer and a semiconductor switch to convert input DC into AC. A boosting section(120) comprises a plurality of diodes and capacitors to boost the AC converted by the flyback conversion section to DC output voltage. A triggering capacitor section(130) charges the output voltage boosted by the boosting section. A switch section(150) comprises a trigger circuit unit(152) to supply or block the output voltage charged by the triggering capacitor section.
申请公布号 KR100763558(B1) 申请公布日期 2007.10.04
申请号 KR20060117707 申请日期 2006.11.27
申请人 KOREA AEROSPACE RESEARCH INSTITUTE 发明人 MA, KEUN SU;LIM, YOU CHOL;KIM, MYUNG HWAN;LEE, JAE DEUK
分类号 B64G1/40;B64G1/42;F42C11/00 主分类号 B64G1/40
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